|Número de publicación||US6123751 A|
|Tipo de publicación||Concesión|
|Número de solicitud||US 09/094,083|
|Fecha de publicación||26 Sep 2000|
|Fecha de presentación||9 Jun 1998|
|Fecha de prioridad||9 Jun 1998|
|También publicado como||DE69921321D1, DE69921321T2, EP1086303A1, EP1086303B1, US6368386, WO1999064735A1|
|Número de publicación||09094083, 094083, US 6123751 A, US 6123751A, US-A-6123751, US6123751 A, US6123751A|
|Inventores||Benny Kevin Nelson, Mark Alan Gogins|
|Cesionario original||Donaldson Company, Inc.|
|Exportar cita||BiBTeX, EndNote, RefMan|
|Citas de patentes (33), Otras citas (8), Citada por (67), Clasificaciones (23), Eventos legales (5)|
|Enlaces externos: USPTO, Cesión de USPTO, Espacenet|
The present invention relates to air filter systems. In certain applications it concerns air filters for use in the air intake stream of gas turbine systems. In specific applications, it concerns filter constructions applied in gas turbine systems which are constructed to resist passage of moisture and/or salt therethrough. Methods of filtering to achieve such effect are also provided.
Although the present invention may be applied in a variety of applications, it was developed for use with gas turbine filter systems. Single stage, self cleaning air filter systems are known. One such system, commercially available, is the Donaldson GDX™ Pulse Cleaning Filter System available from Donaldson Company, Inc., Minneapolis, Minn. In FIG. 1, a schematic, cross-sectional, depiction of a Donaldson GDX™ Pulse Cleaning Filter System 20 is presented.
Referring to FIG. 1, the system 20 includes a chamber 21 having an air inlet side 22 and an air outlet side 23. Air enters the chamber 21 through a plurality of vertically spaced inlet hoods 26 positioned along the air inlet side 22. The inlet hoods 26 function to protect internal filters of the system 20 from the effects of rain, snow and sun. Also, the inlet hoods 26 are configured such that air entering the inlet hoods 26 is first directed in an upward direction indicated by arrow 27, and then deflected by deflector plates 28 in a downward direction indicated by arrow 29. The initial upward movement of air causes some particulate material and moisture from the air stream to settle or accumulate on lower regions 30 of the inlet hoods 26. The subsequent downward movement of air forces dust within the chamber 21 downward toward a dust collection hopper 32 located at the bottom of the chamber 21.
The chamber 21 of the system 20 is divided into upstream and downstream volumes 34 and 36 by a partition 38. The upstream volume 34 generally represents the "dirty air section" of the air cleaner system 20, while the downstream volume generally represents the "clean air section" of the system 20. The partition 38 defines a plurality of apertures 40 for allowing air to flow from the upstream volume 34 to the downstream volume 36. Each aperture 40 is covered by an air filter 42 or filter cartridge located in the upstream volume 34 of the chamber. The filters 42 are arranged and configured such that air flowing from the upstream volume 34 to the downstream volume 36 passes through the filters 42 prior to passing through the apertures 40.
For the particular filter arrangement shown, each air filter 42 includes a pair of filter elements. For example, each air filter 42 includes a cylindrical element 44 and, a somewhat truncated, conical, element 46. Each truncated, conical element 46 includes one end having a major diameter and another end having a minor diameter. The cylindrical element 44 and the truncated, conical element 46 of each filter 42 are co-axially aligned and connected end-to-end with the minor diameter end of each conical element 46 being secured to one of the cylindrical elements 44 in a sealed manner. The major diameter end of each truncated, conical element 46 is secured to the partition 38 such that an annular seal is formed around its corresponding aperture 40. Each filter 42 is generally co-axially aligned with respect to its corresponding aperture 40 and has a longitudinal axis that is generally horizontal.
In general, during filtering, air is directed from the upstream volume 34 radially through the air filters 42 into interior volumes 48 of the filters 42. After being filtered, the air flows from the interior volumes 48 through the partition 38, via apertures 40, into the downstream clean air volume 36. The clean air is then drawn out from the downstream volume 36, through apertures 50, into a gas turbine intake, not shown.
Each aperture 40 of the partition 38 includes a pulse jet air cleaner 52 mounted in the downstream volume 36. Periodically, the pulse jet air cleaner 52 is operated to direct a pulse jet of air backwardly through the associated air filter 42, i.e. from the interior volume 48 of the filter element outwardly to shake or otherwise dislodge particular material trapped in or on the filter media of the air filter 42. The pulse jet air cleaners 52 can be sequentially operated from the top to the bottom of the chamber 21 to eventually direct the dust particulate material blown from the filters into the lower hopper 32, for removal.
Arrangements such as those shown in FIG. 1 may be rather large. Filter pairs used in such arrangements commonly include cylindrical filters that are about 26 inches long and about 12.75 inches in diameter, and truncated conical filters that are about 26 inches long, about 12.75 inches in minor diameter, and about 17.5 inches in major diameter. Such arrangements might be used, for example, for filtering intake air to a gas turbine system having an air flow demand on the order of 8000 to 1.2 million cubic feet per minute (cfm).
A variety of types of filter elements have been used in arrangements such as that described above with respect to FIG. 1. Donaldson Company, Inc., for example, markets filter elements under the designation "GDX filter elements" for such systems which comprise pleated paper having a web of submicron diameter fibers applied to a surface thereof, using proprietary, trade secret, Donaldson method, under the designation Spider-Web ®.
One aspect of the present invention relates to methods and systems that use hydrophobic media to reduce the concentration or amount of water soluble material such as salt present in the intake air of a gas turbine engine or other type of environment that is sensitive to water soluble materials such as salt.
Another aspect of the present invention relates to a gas turbine intake air filter system including a first stage air cleaner for reducing the concentration of particulate material in the turbine intake air, and a second stage filter arrangement located downstream from the first stage air cleaner. The second stage filter arrangement includes a hydrophobic medium arranged and configured to reduce the concentration of moisture/salt solution in the intake air.
A further aspect of the present invention relates to a barrier arrangement for filtering water soluble material such as salt from an air stream such that the concentration of water soluble material is reduced. The barrier arrangement includes a plurality of vertically spaced-apart hydrophobic filter elements. The barrier arrangement also includes a plurality of inclined baffles arranged and configured to direct the air stream upward through the hydrophobic filter elements. Each of the baffles is positioned beneath a corresponding one of the hydrophobic filter elements. In operation, salt solution accumulates on lower surfaces of the filter elements. The accumulated salt solution drips from the filter elements onto the inclined baffles. The inclination of the baffles causes the salt solution to run downward and drip off upstream edges of the baffles.
An additional aspect of the present invention relates to a gas turbine system including a gas turbine adapted to draw intake air. The system also includes a hydrophobic medium through which the intake air is filtered prior to entering the gas turbine.
Still another aspect of the present invention relates to a method for filtering intake air of a gas turbine. The method includes the steps of filtering particulate material from the intake air at a first stage air cleaner, and directing the intake air downstream from the first stage air cleaner through an air flow gap to a second stage salt barrier. The method also includes the steps of reducing the concentration or level of salt in the intake air at the second stage salt barrier, and directing the intake air downstream from the second stage salt barrier to the gas turbine.
One further aspect of the present invention relates to a filter including a pleated filter element having a plurality of pleat tips, and an elastic member having portions that straddle the pleat tips and portions that extend between the pleat tips to maintain pleat spacing. In certain embodiments, the elastic member comprises a coil spring having a plurality of coils positioned between the pleat tips for maintaining pleat spacing of the pleated filter element.
A variety of advantages of the invention will be set forth in part in the description which follows, and in part will be apparent from the description, or may be learned by practicing the invention. It is to be understood that both the foregoing general description and the following detailed description are explanatory only and are not restrictive of the invention as claimed.
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate several aspects of the invention and together with the description, serve to explain the principles of the invention. A brief description of the drawings is as follows:
FIG. 1 is a schematic cross-sectional view of a prior art gas turbine intake filtration system;
FIG. 2 is a schematic cross-sectional view of a gas turbine intake filtration system constructed in accordance with the principles of the present invention;
FIG. 3 is a schematic view of an illustrative salt barrier arrangement constructed in accordance with the principles of the present invention;
FIG. 4 is a perspective view of the salt barrier arrangement of FIG. 3; and
FIG. 5 is a cross-sectional view taken along section line 5--5 of FIG. 4.
While various aspects of the present invention are described primarily with respect to gas turbine intake systems, it will be appreciated that the aspects of the present application are also applicable to a variety of other environments that are sensitive to contamination by water soluble materials such as salt. For example, the various aspects of the present invention are applicable to alternative environments such as internal combustion engine intake systems, fuel cell intake systems, clean room intake systems, heating ventilating and air conditioning (HVAC) systems, hospital HVAC systems, air compressor intake systems, clean chamber intake systems (mini-clean room boxes), clean benches and industrial process exhaust filtration.
A. Salt Particles as Contaminant in Gas Turbine Intake Systems
In marine environments, such as offshore environments or seaside environments, airborne salt is generated by wave breaking and is carried by the wind Particle sizes are generally reported to be from submicron up to about 20 microns. In other environments, such as deserts and environments proximate industrial discharges, relatively high concentrations of salt are also present in the air. Salt particles carried in the air are generally salts, such as NaCl, KCl. However, other chemical salts such as ammonium sulfates, magnesium sulfate or other sulfates may also be carried in the air. In general terms, the word "salt" is intended to mean any particulate, contaminate or material that deliquesces or changes physical state with varying humidity conditions. The term "salt" is also intended to mean any material or contaminant that is soluble in water.
High salt concentrations in the air present problems for gas turbine systems. For example, if salt passes through the intake air filter system of a gas turbine system, the salt can coat the ducting and foul the compressor blades of the turbine system. This leads to significant power losses.
Salt particles can penetrate the filter media of filter cartridges, such as those described in connection with FIG. 1 above, in several manners. For example, if the particles are sufficiently small, they can pass through the filter media due to particle size and efficiency of the media. However, a more significant migration of salt through the filter material occurs as a result of moisture contamination.
Moisture contamination is particularly problematic in environments having relatively high humidities such as marine environments. Specifically, if the air passing into an air filtration system is relatively humid, salt collected on the filter elements will go into solution, and then migrate through the filter media When the salt solution reaches the downstream side of the filter media, the salt solution is carried by the air flow stream through the clean air plenum and into downstream duct work, toward the gas turbine. This type of salt migration can cause substantial problems with gas turbine operations and is a particular problem addressed by techniques according to the present invention. It is noted that the techniques described in the present disclosure are also useful with respect to salt migrations that occur in similar manners involving contaminant phase changes with respect to humidity.
B. A General Approach To Inhibiting Salt Deposition on Downstream Ductwork and Gas Turbine Equipment-A Second Stage Moisture/Salt Barrier Construction
According to the present disclosure, an approach to inhibiting salt solution migration through filter cartridges in air intake filter systems is provided. The approach generally involves the provision, downstream of the filter cartridges, of a second stage barrier. The barrier generally comprises a secondary air filter comprising at least in part a hydrophobic media. A preferred hydrophobic media is microporous polytetrafluorethylene (PTFE) membrane comprising nodes interconnected by fibers. Such membranes are commercially available from such sources as Tetratec, a division of Donaldson Company, Inc., the assignee of the present invention, under the designation Tetratex®; and from W. L Gore & Associates, under the designation Gore Text®. Preparation of such membranes is described in such references as U.S. Pat. Nos. 5,362,553, 5,157,058, 5,066,683,4,945,125, 4,187,390, and 3,953,566, which are incorporated herein by reference.
Typical moisture/salt barrier media used in arrangements according to the present invention will comprise a laminate of hydrophobic membrane, such as a microporous polytetrafluorethylene (PTFE) membrane, applied to a support substrate such as an open fibrous supporter scrim made of a material such as a polyester felt. A useable such laminate is a hydrophobic membrane applied to a 6 oz. polyester scrim available, for example, from Reemay Inc. of Charleston, S.C. Such a laminate is commercially available from the Tetratec division of Donaldson Company, Inc., under the designation Tetratex® 6279.
It will be appreciated that a variety of filtering configurations and materials can be used to reduce the concentration or level of moisture and deliquesced salt present in an air stream. By way of non-limiting example, illustrative hydrophobic/moisture filtering materials or fibers include polytetrafiuoroethylene, polypropylene, polyethylene, polyvinyl chloride, polysulfone and polystyrene. Materials and fibers can also be made hydrophobic through the use of surface treatments. Illustrative surface treatments include fluorocarbons and silicones. Of course, the particular hydrophobic materials listed herein are strictly examples, and other materials can also be used in accordance with the principles of the present invention.
In certain embodiments of the present invention, the second stage filter laminate will be used in a pleated configuration, with a pleat space of about 6-8 pleats per inch, or 4-10 pleats per inch, or at least 3 pleats per inch. Typical preferred constructions will comprise rectangular panel filters, with pleats extending across a length or width of each panel. An example of such a panel filter is illustrated in FIG. 4, described below. A pleat depth of at least about 1/4 inches, generally no greater than about 12 inches, and typically about 1 to 4 inches will be preferred. A preferred pore size of the filter media is about 3 microns. An air permeability of at least 4 cfm, generally no greater than 100 cfm, and typically about 7-10 cfm will be preferred. A preferred hydrophobic membrane thickness is about 0.4 mil, while a preferred media thickness, including both membrane and scrim, is in the range of 0.01-0.05 inches. While a pleated filter configuration is preferred, alternative configurations such as Z-configuration filters can also be used.
It is foreseen that in typical gas turbine systems, the second stage construction will be arranged such that the media velocity will be about 4-12 feet per minute (fpm), or about 5-15 fpm, or about 5-40 fpm. More particularly, the media velocity is preferably about 9 fpm, and typically no greater than about 20 fpm. The term "media velocity" in this context refers to the volume of flow through the filter media per unit surface area of filter media. It is also foreseen that in typical gas turbine systems, the second stage construction will be arranged such that the perimeter velocity will be about 500-900 feet per minute (fpm), and typically no greater than about 1000 fpm. The term "perimeter velocity" in this context refers to the volume of flow through the filter media per perimeter area of filter media. Hence, the perimeter velocity does not take into consideration extra area provided by means such as pleating.
FIG. 2 is a schematic cross sectional depiction of a gas turbine intake system 54 including an arrangement according to the present invention. Generally, the system 54 includes a two-stage filtration system for removing both particulate material and airborne salt from intake air drawn through the system to a gas turbine 64. Small gas turbine systems can have air flow demands in the neighborhood of 8000 cfm, while large gas turbine systems can intake air at rates as large as 1.2 million cfm.
The system 54 includes a first stage air cleaner 20', and a second stage salt barrier arrangement 60 positioned downstream from the first stage air cleaner 20'. Ductwork 62 directs filtered air from the salt barrier arrangement 60 to the gas turbine 64.
The first stage air cleaner 20' has a similar configuration to the filtration system 20 depicted in FIG. 1. For example, the first stage cleaner 20' includes a chamber 21' having an air inlet side 22' and an air outlet side 23'. Air enters the chamber 21' through a plurality of vertically spaced inlet hoods 26' positioned along the air inlet side 22'. The chamber 21' of the cleaner 20' is divided into upstream and downstream volumes 34' and 36' by a partition 38'. The upstream volume 34' generally represents the "dirty air section" of the air cleaner 20', while the downstream volume 36' generally represents the "clean air section" of the air cleaner 20'.
The partition 38' defines a plurality of apertures 40' for allowing air to flow from the upstream volume 34' to the downstream volume 36'. Filters 42' or filter cartridges are arranged and configured such that air flowing from the upstream volume 34' to the downstream volume 36' is required to pass through the filters 42' prior to passing through the apertures 40'. The apertures 40' of the partition 38' include pulse jet air cleaners (not shown) for periodically cleaning the filters via backpressure.
It will be appreciated that for small scale operations, as few as one filter 42' and one aperture 40' may be used. By contrast, large scale operation may require hundreds of filter elements 42' and apertures 40'. Also, while filter systems having jet air cleaners are preferred, static systems can also be used. Additionally, other air cleaning configurations can also be used to clean air at the first stage. For example, panel filters, inertial separators, water wash systems, and other techniques for removing particulate materials can also be used.
In general, during filtering, air is directed from the upstream volume 34' radially through the air filters 42' into interior volumes of the filters 42'. After being filtered, the air flows from the interior volumes of the filters 42' through the partition 38', via apertures 40', into the downstream clean air volume 36'. The clean air is then drawn out from the downstream volume 36', through apertures 50', into the second stage salt barrier arrangement 60.
The air filters 42' preferably include a cellulose or synthetic filter media arranged in a pleated configuration. In certain embodiments, a web of sub-micron diameter fibers, such as Spider-Web® Filter Media available from Donaldson Company, is bonded to the outer surface of the filter media It is foreseen that in typical gas turbine systems, the first stage construction will be arranged such that the media velocity will be in the range of 1-5 feet per minute (fpm), and typically no greater than about 5 fpm.
The first stage air cleaner 20' preferably has relatively high filtering efficiencies with respect to particulate material. For example, filters having initial filtration efficiencies in the range of 65-75%, or greater than 65% can be used. Filtration efficiencies are preferably determined using American Society for Testing and Materials (ASTM) standard test ASTM F1215-89 for determining the initial efficiency of a flatsheet filter medium in an airflow using latex spheres. Preferably the test is conducted with a single particle size of 0.76 micrometers and a single face velocity of 20 feet per minute. It will also be appreciated that for some applications, it may be desirable to use air cleaners having filtration efficiencies other than those specified above.
Referring back to FIG. 2, the second stage salt barrier arrangement 60 is located immediately downstream from the first stage air cleaner 20' and functions to reduce the concentration of deliquesced salt in the air that exits the first stage air cleaner 20'. The barrier arrangement 60 includes an upstream volume or side 66 and a downstream volume or side 68. A substantially vertical rack 70 is positioned between the upstream and downstream sides 66 and 68. The clean air volume 36' and the upstream volume 66 preferably form an air flow gap between the first stage air cleaner 20' and the second stage salt barrier arrangement 60. The outlet side 23' can include a wall defining apertures similar to the outlet side 23 of FIG. 1, or can be open to promote substantially unrestricted flow between the clean air volume 36' and the volume 66.
A plurality of filter modules 72 are mounted on the rack in a vertically stacked relationship. Each of the filter modules 72 includes a filter medium, such as the hydrophobic filter medium described previously, adapted for removing or filtering salt and moisture from the air stream such that the concentration of salt solution in the intake air is reduced. The filter modules 72 are mounted in a sealed relation with respect to the rack 70 such that air from the upstream side 66 is required to pass through a filter medium to reach the downstream side 68.
FIG. 3 shows a schematic view of one of the filter modules 72. The filter module 72 includes a front side aligned along a substantially vertical front plane A, and a back side aligned along a substantially vertical back plane B. A plurality of filter elements 74 are positioned between the front and back planes A and B. The filter elements 74 are vertically stacked in a spaced-apart and substantially parallel relationship. Each filter element 74 is aligned along a generally horizontal plane. A preferred vertical spacing s between the filter elements 74 is in the range of 1 to 6 inches.
The filter elements 74 preferably include a plurality of pleats 75 (shown in FIG. 4), and are preferably constructed of a pleated hydrophobic material. As shown in FIG. 4, the pleats are aligned generally parallel with respect to the direction of air flow (shown by arrow 77). However, it will be appreciated that in alternative embodiments, the pleats can be aligned perpendicular to or at oblique angles with respect to the direction of air flow as indicated by arrow 77.
As best shown in FIG. 4, each filter element 74 is preferably mounted in a generally rectangular frame 76. The frames 76 and filter elements 74 together form generally horizontal, vertically stacked filter shelves or panels. Potting material preferably provides a seal about the perimeter of each filter element 74 and functions to secure the filter elements 74 to their corresponding frame 76. Upstream ends of the frames 76 are preferably secured to a generally rectangular mounting flange 87 for use in connecting or clamping the module 72 to the rack 70. The module 72 also includes first and second sets of side wall pieces 73 (only one of the sets of side wall pieces is shown in FIG. 4) that extend generally between the front and back sides of the module 72. As shown in FIG. 4, the side wall pieces 73 include truncated triangular pieces. Single piece continuous side walls can also be used.
Referring back to FIG. 3, an inclined baffle 78 is located beneath each filter element 74. The baffles 78 extend between the front and back planes A and B and are preferably aligned at an angle in the range of 5 to 30 degrees, or at least 2 degrees, with respect to horizontal. As shown in FIG. 3, the baffles 78 extend between upstream and downstream ends of the frames 76, and are substantially parallel and generally planar. For example, each baffle 78 has a upstream edge 82 located generally at the front plane A and a downstream edge 83 located generally at the back plane B. The baffles 78 incline in a direction extending from the front plane A to the back plane B such that the upstream edge 82 of each baffle 78 is lower than the downstream edge 83 of each baffle 78.
Preferably, the baffles 78 also extend between the side walls 73 of the module 72. As shown in FIG. 4, each side wall piece 73 extends upward from one of the baffles 78 to a corresponding filter panel positioned directly above the baffle 78.
The baffles 78 are arranged and configured to direct the air stream upward through the filter elements 74 and to inhibit air from by-passing the filter elements 42. As shown in FIG. 3, the baffles 78 extend between the filter elements 74 across the vertical gaps or spacing s that exists between the filter elements 74. The baffles 78 are also arranged and configured to direct the air that flows upward through the filter elements 74 outward through the back plane B of the module 72. By deflecting the air that enters and exits the module 72, uniform flow through the filter elements 74 is encouraged.
Referring again to FIG. 3, the upstream side 66 is located on the left side of the filter module 72, while the downstream side 68 is located on the right side of the filter module 72. As shown by arrows 77, air enters the module 72 through the front plane A. As the air enters the module 72, the air is directed upward (shown by arrows 80) through the filter elements 74 by top surfaces of the inclined baffles 78. After passing through the filter elements 74, the air stream is directed out the back plane B of the module 72 by bottom sides of the baffles 78. Arrows 85 represent the air exiting the module 72.
When air flows upward through the filter elements 74, deliquesced salt accumulates on bottom surfaces/upstream portions of the filters 74 and drips down onto the top surfaces of the baffles 78. The inclination of the baffles 78 is preferably sufficiently steep to cause the salt solution to run downward, against the direction of air flow, and drip off the upstream edges 82 of the baffles 80. A collection basin or drain is preferably located at the bottom of the second stage salt barrier arrangement 60 for collecting the salt solution that is removed from the air stream by the filter elements 74. Air that passes through the filter elements 74 is directed toward the ductwork 62 and flows through the ductwork 62 to the gas turbine 64.
In operation, air enters the gas turbine intake system 54 through the inlet hoods 26' and is directed in a downward direction into the upstream "dirty air" volume 34'. The air then flows from the upstream volume 34' to the downstream volume 36' through the air filters 42'. The air filters 42' remove a large percentage of the particulate material from the air stream such that the air entering the downstream volume 36' is substantially clean. However, in certain environments, salt can migrate or otherwise pass through the filters 42'. Consequently, to reduce the concentration of salt that may be present in the air stream after the first stage filtration, the air is passed through a second stage filtration step in the form of the salt barrier arrangement 60. As the air passes upward through the filter elements 74 of the salt barrier arrangement 60, salt solution accumulates on the upstream sides of the filter elements 74 and drips onto the inclined baffles 78. The salt solution then drips off the baffles 78 and is collected in a basin or drain at the bottom of the salt barrier arrangement 60. As a result, air passing through the filter elements 74 is preferably substantially free of salt. Hence, salt is inhibited from being deposited or accumulating on subsequent intake ductwork 62 or on compressor blades of the turbine system.
In general, a preferred moisture/salt barrier construction would include media as generally characterized hereinabove, to inhibit passage of moisture and salt therethrough. Because a first stage filtration step is used to efficiently filter particulate material, in certain embodiments, the salt barrier construction can use small pore sizes and can also use a static media system.
Another aspect of the present invention relates to a technique for maintaining pleat spacing and/or pleat shape in a pleated filter. Generally, the aspect relates to using bent wires or other elongated elastic members having portions that straddle the pleat tips of a pleated filter, and portions that extend between the pleats for maintaining pleat spacing. For example, as shown in FIGS. 3 and 4, the filter elements 42 include helical coils 96 or springs for maintaining pleat spacing and pleat shape. As shown in FIG. 5, separate pleat tips 75 of the filter element 42 are positioned between consecutive coils 100 of the helical coil 96. Also, portions of one or more of the coils 100 are positioned between consecutive pleat tips 75 of the filter element 42, and portions of the coils 100 straddle the pleat tips 75. By varying the number of coils 100 positioned between consecutive pleat tips 75, a desired spacing between the pleat tips can also be varied. The pleat tip spacing and pleat shape can further be varied by using coils having different spring pitches, diameters and wire diameters. Furthermore, the coils can be made of a variety of materials such as metal or plastic. Additionally, coils formed by wires or members having non-round cross sections can also be used.
While FIGS. 4 and 5 illustrate springs used in association with pleated panel filters, it will be appreciated that coils can also be used for maintaining pleat spacing in other types of pleated filters such as pleated cylindrical filters. Furthermore, coils can be used for maintaining pleat shape. For example, coils can be used to control or inhibit pleat bagging or figure-8 pleats. Also, while coils or other wire/elastic member configurations are shown or described for maintaining pleat spacing, other known techniques such as spacing beads, spacing strips, or spacing bumps/projections formed on the filter medium itself can also be used.
The above specification, examples and data provide a complete description of the manufacture and use of the composition of the invention. Since many embodiments of the invention can be made without departing from the spirit and scope of the invention, the invention resides in the claims hereinafter appended.
|Patente citada||Fecha de presentación||Fecha de publicación||Solicitante||Título|
|US3243943 *||15 Jun 1964||5 Abr 1966||American Air Filter Co||Unit filter construction|
|US3511337 *||16 Ene 1968||12 May 1970||American Mach & Foundry||Gas turbine noise attenuator|
|US3631654 *||3 Oct 1968||4 Ene 1972||Baxter Laboratories Inc||Gas purge device|
|US3828524 *||9 Ago 1971||13 Ago 1974||Nasa||Centrifugal lyophobic separator|
|US3853529 *||9 Jun 1971||10 Dic 1974||Farr Co||Pleated air filter cartridge|
|US3950157 *||7 Oct 1974||13 Abr 1976||Dorrance Henry Matney||Ram air filter for light aircraft|
|US3953566 *||3 Jul 1973||27 Abr 1976||W. L. Gore & Associates, Inc.||Process for producing porous products|
|US4004899 *||28 Feb 1975||25 Ene 1977||Alfred Giacovas||Air filter construction|
|US4135900 *||31 May 1977||23 Ene 1979||American Air Filter Company, Inc.||Gas filter device|
|US4158449 *||7 Dic 1976||19 Jun 1979||Pall Corporation||Inlet air cleaner assembly for turbine engines|
|US4187390 *||21 Jun 1977||5 Feb 1980||W. L. Gore & Associates, Inc.||Porous products and process therefor|
|US4234323 *||29 Sep 1978||18 Nov 1980||United Technologies Corporation||Collector for water separator|
|US4300918 *||10 Mar 1980||17 Nov 1981||Parmatic Filter Corporation||Method for removing moisture particles|
|US4452616 *||1 Abr 1982||5 Jun 1984||Donaldson Company, Inc.||Self-cleaning air cleaner|
|US4504293 *||28 Jun 1983||12 Mar 1985||Donaldson Company, Inc.||Self-cleaning air filter|
|US4619675 *||22 Jun 1984||28 Oct 1986||Midori Anzen Co., Ltd.||Filter for air cleaners|
|US4652285 *||19 Oct 1983||24 Mar 1987||Greene John P||Gas filter apparatus|
|US4878930 *||15 Mar 1984||7 Nov 1989||W. L. Gore & Associates, Inc.||Filter cartridge|
|US4945125 *||5 Ene 1987||31 Jul 1990||Tetratec Corporation||Process of producing a fibrillated semi-interpenetrating polymer network of polytetrafluoroethylene and silicone elastomer and shaped products thereof|
|US5026591 *||14 Abr 1989||25 Jun 1991||W. L. Gore & Associates, Inc.||Coated products and methods for making|
|US5066683 *||1 May 1990||19 Nov 1991||Tetratec Corporation||Microporous waterproof and moisture vapor permeable structures, processes of manufacture and useful articles thereof|
|US5157058 *||7 Jun 1991||20 Oct 1992||Tetratec Corporation||Microporous waterproof and moisture vapor permeable structures, processes of manufacture and useful articles thereof|
|US5350515 *||29 Mar 1993||27 Sep 1994||W. L. Gore & Associates, Inc.||Internally potted end cap for a pleated filter medium|
|US5362553 *||27 Ago 1993||8 Nov 1994||Tetratec Corporation||Microporous waterproof and moisture vapor permeable fabric|
|US5397632 *||14 May 1993||14 Mar 1995||Reemay, Inc.||Nonwoven laminated composite article capable or readily undergoing pleating to form a stable pleated depth gaseous filtration medium|
|US5403367 *||24 Feb 1993||4 Abr 1995||Atomic Energy Corporation Of South Africa Limited||Filtration|
|US5478372 *||8 Feb 1995||26 Dic 1995||W. L. Gore & Associates, Inc.||High temperature, chemical resistant laminate for filtration systems|
|US5562746 *||27 Sep 1995||8 Oct 1996||Donaldson Company, Inc.||Air filter assembly for filtering air with particulate matter|
|US5653786 *||20 Dic 1995||5 Ago 1997||Peerless Manufacturing Company||High capacity marine separator|
|US5820645 *||23 May 1997||13 Oct 1998||Reemay, Inc.||Pleatable nonwoven composite article for gas filter media|
|US5853439 *||27 Jun 1997||29 Dic 1998||Donaldson Company, Inc.||Aerosol separator and method|
|*||USB14395269||Título no disponible|
|WO1995005234A1 *||16 Ago 1994||23 Feb 1995||Donaldson Co Inc||Mist collector cartridge|
|1||"GDX™ Pulse Cleaning Filter System." Donaldson® Gas Turbine Systems Brochure #3000-46,4 pgs. (Copyright 1996).|
|2||"Genuine Duralife™ Filter Cartridges From Donaldson." Bulletin 3000-33, 4 pgs, Available to public prior to filing date.|
|3||"Spider-Web® Filter Media." Donaldson® Gas Turbine Systems Brochure #3000-35, 4 pgs. (Copyright 1994).|
|4||"The New GDX™ Self-Cleaning Air Filter From Donaldson." Bulletin 3000-31, 4 pgs, Available to public prior to filing date.|
|5||*||GDX Pulse Cleaning Filter System. Donaldson Gas Turbine Systems Brochure 3000 46,4 pgs. (Copyright 1996).|
|6||*||Genuine Duralife Filter Cartridges From Donaldson. Bulletin 3000 33, 4 pgs, Available to public prior to filing date.|
|7||*||Spider Web Filter Media. Donaldson Gas Turbine Systems Brochure 3000 35, 4 pgs. (Copyright 1994).|
|8||*||The New GDX Self Cleaning Air Filter From Donaldson. Bulletin 3000 31, 4 pgs, Available to public prior to filing date.|
|Patente citante||Fecha de presentación||Fecha de publicación||Solicitante||Título|
|US6302932 *||10 Nov 1999||16 Oct 2001||Honeywell International, Inc.||Combined water coalescer odor removal filter for use in water separation systems|
|US6368386 *||10 Jul 2000||9 Abr 2002||Donaldson Company, Inc.||Filter construction resistant to the passage of water soluble materials; and method|
|US6500038 *||29 Oct 2001||31 Dic 2002||Brunswick Corporation||Passive air vent system for a marine propulsion engine|
|US6550347||30 Nov 2000||22 Abr 2003||Bruce J. Bradley||Vacuum air component sampler|
|US6673136||31 May 2001||6 Ene 2004||Donaldson Company, Inc.||Air filtration arrangements having fluted media constructions and methods|
|US6716274||31 May 2001||6 Abr 2004||Donaldson Company, Inc.||Air filter assembly for filtering an air stream to remove particulate matter entrained in the stream|
|US6740142||31 May 2001||25 May 2004||Donaldson Company, Inc.||Industrial bag house elements|
|US6743273||31 May 2001||1 Jun 2004||Donaldson Company, Inc.||Polymer, polymer microfiber, polymer nanofiber and applications including filter structures|
|US6746517||31 May 2001||8 Jun 2004||Donaldson Company, Inc.||Filter structure with two or more layers of fine fiber having extended useful service life|
|US6800117||31 May 2001||5 Oct 2004||Donaldson Company, Inc.||Filtration arrangement utilizing pleated construction and method|
|US6875256||10 Dic 2003||5 Abr 2005||Donaldson Company, Inc.||Methods for filtering air for a gas turbine system|
|US7048500 *||1 Mar 2004||23 May 2006||Donaldson Company, Inc.||Silencer for ventilation system and methods|
|US7048501 *||21 Nov 2001||23 May 2006||Mitsubishi Heavy Industries, Ltd.||Dust collecting filter, dust collecting device, and air intake device for gas turbine|
|US7217184 *||24 Abr 2006||15 May 2007||Mjd Innovations, L.L.C.||Electrical generator fluid-flow-coolant filtration method|
|US7297173||30 Nov 2004||20 Nov 2007||Donaldson Company, Inc.||Gas turbine air intake system with bypass arrangement and methods|
|US7632339||18 Dic 2006||15 Dic 2009||General Electric Company||Moisture removal apparatus and method|
|US7959699 *||20 Sep 2007||14 Jun 2011||Lennox Industries Inc.||Collapsible filter with folding arms|
|US8029588||1 Dic 2010||4 Oct 2011||Donaldson Company, Inc.||Fine fiber media layer|
|US8075674 *||29 Nov 2007||13 Dic 2011||Donaldson Company, Inc.||Filter apparatus with pulse cleaning and methods for pulse cleaning filters|
|US8118901||30 Oct 2009||21 Feb 2012||Donaldson Company, Inc.||Fine fiber media layer|
|US8167980 *||28 Ago 2008||1 May 2012||General Electric Company||Filtration system for gas turbines|
|US8182587 *||28 Ago 2008||22 May 2012||General Electric Company||Filtration system for gas turbines|
|US8234874||9 Oct 2009||7 Ago 2012||General Electric Company||Systems and methods for bypassing an inlet air treatment filter|
|US8349043 *||11 Feb 2011||8 Ene 2013||General Electric Company||Turbine inlet air system|
|US8349044||3 Nov 2011||8 Ene 2013||Donaldson Company, Inc.||Filter apparatus with pulse cleaning and methods for pulse cleaning filters|
|US8366797||17 Ago 2011||5 Feb 2013||Donaldson Company, Inc.||Fine fiber media layer|
|US8475115||2 Jun 2010||2 Jul 2013||General Electric Company||Pre-filtration bypass for gas turbine inlet filter house|
|US8512431||12 Sep 2012||20 Ago 2013||Donaldson Company, Inc.||Fine fiber media layer|
|US8661831||15 Ene 2010||4 Mar 2014||Bha Altair, Llc||Adaptive gas turbine vane separator system and method|
|US8673040||11 Jun 2009||18 Mar 2014||Donaldson Company, Inc.||Filter construction for use with air in-take for gas turbine and methods|
|US8709118||10 Ene 2013||29 Abr 2014||Donaldson Company, Inc.||Fine fiber media layer|
|US8721756||14 Sep 2012||13 May 2014||Donaldson Company, Inc.||Filter construction for use with air in-take for gas turbine and methods|
|US8728401||26 Oct 2009||20 May 2014||Sefar BDH, Inc.||Filter bag, pleatable filtration material therefore, and process of making same|
|US8936660 *||31 May 2013||20 Ene 2015||Jorge Andres CRUZ AGUADO||Ventilation screen|
|US9016065||14 Feb 2011||28 Abr 2015||Donaldson Company, Inc.||Coil arrangement for air intake system for gas turbine and methods|
|US9114347||7 Jun 2013||25 Ago 2015||Bha Altair, Llc||Moisture separation system for high efficiency filtration|
|US20020046656 *||31 May 2001||25 Abr 2002||Benson James D.||Filter structure with two or more layers of fine fiber having extended useful service life|
|US20040060269 *||30 Sep 2003||1 Abr 2004||Donaldson Company, Inc.||Polymer, polymer microfiber, polymer nanofiber and applications including filter structures|
|US20040103626 *||12 Ago 2003||3 Jun 2004||Warth Scott B.||Filter element, filter assembly, gas turbine system, and methods|
|US20040141835 *||21 Nov 2001||22 Jul 2004||Hiroyuki Katayama||Dust collecting filter, dust collecting device, and intake device of gas turbine|
|US20040187454 *||14 Ene 2004||30 Sep 2004||Donaldson Company, Inc.||Polymer, polymer microfiber, polymer nanofiber and applications including filter structures|
|US20040200354 *||3 May 2004||14 Oct 2004||Donaldson Company, Inc.||Filtration arrangement utilizing pleated construction and method|
|US20040226443 *||10 Dic 2003||18 Nov 2004||Donaldson Company, Inc.||Methods for filtering air for a gas turbine system|
|US20050183405 *||20 Abr 2005||25 Ago 2005||Donaldson Company, Inc.||Air filtration arrangements having fluted media construction and methods|
|US20050191169 *||1 Mar 2004||1 Sep 2005||Cuvelier Leon R.||Silencer for ventilation system and methods|
|US20060112825 *||30 Nov 2004||1 Jun 2006||Dominique Renwart||Gas turbine air intake system with bypass arrangement and methods|
|US20060192049 *||24 Abr 2006||31 Ago 2006||Mjd Innovations, L.L.C.||Electrical generator fluid-flow-coolant filtration method|
|US20060196359 *||25 Abr 2006||7 Sep 2006||Donaldson Company, Inc.||Air filtration arrangements having fluted media constructions and methods|
|US20070012007 *||19 Jul 2004||18 Ene 2007||Donaldson Company, Inc.||Polymer, polymer microfiber, polymer nanofiber and applications including filter structures|
|US20080010959 *||18 Sep 2007||17 Ene 2008||Donaldson Company, Inc.||Air filtration arrangements having fluted media constructions and methods|
|US20080127827 *||29 Nov 2007||5 Jun 2008||Raether Thomas D||Filter apparatus with pulse cleaning and methods for pulse cleaning filters|
|US20080141636 *||18 Dic 2006||19 Jun 2008||Bha Group, Inc.||Moisture removal apparatus and method|
|US20090077937 *||20 Sep 2007||26 Mar 2009||Roger Privitt||Collapsible filter with folding arms|
|US20100050873 *||28 Ago 2008||4 Mar 2010||General Electric Company||Filtration system for gas turbines|
|US20100054919 *||28 Ago 2008||4 Mar 2010||General Electric Company||Filtration system for gas turbines|
|US20110048228 *||11 Jun 2009||3 Mar 2011||Handley Michael W||Filter construction for use with air in-take for gas turbine and methods|
|US20110083419 *||14 Abr 2011||Siddharth Upadhyay||Systems and methods for bypassing an inlet air treatment filter|
|US20110173986 *||21 Jul 2011||Etienne Rene Jarrier||Adaptive Gas Turbine Vane Separator System and Method|
|US20110197592 *||18 Ago 2011||Theodore Philip Bezat||Coil arrangement for air intake system for gas turbine and methods|
|US20120204568 *||16 Ago 2012||General Electric Company||Turbine Inlet Air System|
|US20130319242 *||31 May 2013||5 Dic 2013||Jorge Andres CRUZ AGUADO||Ventilation screen|
|US20140251143 *||6 Mar 2014||11 Sep 2014||Donaldson Company, Inc.||Filtration system for a gas turbine air intake and methods|
|US20140262196 *||13 Mar 2013||18 Sep 2014||Andrew Frank||Thermostat|
|CN101660449B||28 Ago 2009||15 Oct 2014||Bha阿尔泰尔有限责任公司||用于燃气涡轮机的过滤系统|
|CN102076397B *||12 Jun 2009||27 May 2015||唐纳森公司||Filter construction for use with air in-take for gas turbine and methods|
|WO2002020134A2 *||10 Ago 2001||14 Mar 2002||Donaldson Co Inc||Methods for filtering air for a gas turbine system|
|WO2009152439A1 *||12 Jun 2009||17 Dic 2009||Donaldson Company, Inc.||Filter construction for use with air in-take for gas turbine and methods|
|Clasificación de EE.UU.||95/268, 55/528, 55/327, 95/287, 55/501, 55/497, 55/324, 55/332, 55/302, 55/350.1, 55/306, 55/521|
|Clasificación internacional||F02C7/052, B01D46/52, B01D46/12, B01D29/07, B01D50/00|
|Clasificación cooperativa||B01D46/10, B01D46/002, B01D46/523|
|Clasificación europea||B01D46/52F4, B01D46/00D2, B01D46/10|
|9 Jun 1998||AS||Assignment|
Owner name: DONALDSON COMPANY, INC., MINNESOTA
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:NELSON, BENNY KEVIN;GOGINS, MARK ALAN;REEL/FRAME:009240/0409
Effective date: 19980608
|13 Ago 2002||CC||Certificate of correction|
|15 Mar 2004||FPAY||Fee payment|
Year of fee payment: 4
|21 Feb 2008||FPAY||Fee payment|
Year of fee payment: 8
|27 Ene 2012||FPAY||Fee payment|
Year of fee payment: 12